NEW YORK
METROPOLITAN
UNIVERSITY

Undergraduate Certificate in Engineering in Aerospace Engineering

  • Eligibility Criteria

    High school diploma, GED or equiv. International Education

  • Credit Hours

    18

  • Courses Offered

    3

  • Course Duration

    2 Months (Self-Paced) Program

  • Estimated Fee

    $2,340

Courses Offered

An undergraduate certificate offered by NYMU guarantees endless opportunities that will secure your path of career elevation. The certifications allow you to expand your skill set and increases prospects of growth in your career.

Introduction To Propulsion (AEE-152)

TOPICS COVERED IN THIS COURSE
  In Section 1 of this course you will cover these topics:
     The Jet Propulsion Principle
     Mechanics And Thermodynamics Of Fluid Flow
     Steady One-Dimensional Flow Of A Perfect Gas
  In Section 2 of this course you will cover these topics:
     Boundary Layer Mechanics And Heat Transfer
     Thermodynamics Of Aircraft Jet Engines  
     Aerodynamics Of Inlets, Combustors, And Nozzles
  In Section 3 of this course you will cover these topics:
     Axial Compressors
     Axial Turbines
     The Centrifugal Compressor
  In Section 4 of this course you will cover these topics:
     Performance Of Rocket Vehicles
     Chemical Rocket Thrust Chambers
  In Section 5 of this course you will cover these topics:
     Chemical Rocket Propellants: Combustion And Expansion
     Turbomachinery For Liquid-Propellant Rockets
     Electrical Rocket Propulsion

Gas Dynamics (AEE-273)

TOPICS COVERED IN THIS COURSE
  In Section 1 of this course you will cover these topics:
     Basic Equations Of Compressible Flow
     Wave Propagation In Compressible Media
     Isentropic Flow Of A Perfect Gas
  In Section 2 of this course you will cover these topics:
     Stationary Normal Shock Waves
     Moving Normal Shock Waves
     Oblique Shock Waves
  In Section 3 of this course you will cover these topics:
     Pr And Tl Meyer Flow
     Applications Involving Shocks And Expansion Fans
     Flow With Friction
  In Section 4 of this course you will cover these topics:
     Heat Addition
     Equations Of Motion For Multidimensional Flow
     Linearized Flow
  In Section 5 of this course you will cover these topics:
     Methods Of Characteristics
     Computational Gas Dynamics
     Differential Analysis Of Fluid Flow

Introduction To Aerodynamics (AEE-349)

TOPICS COVERED IN THIS COURSE
  In Section 1 of this course you will cover these topics:
     Fluid Properties
     Fundamentals Of Fluid Mechanics
     Dynamics Of An Incompressible, Inviscid Flow Field
  In Section 2 of this course you will cover these topics:
     Viscous Boundary Layers
     Characteristic Parameters For Airfoil And Wing Aerodynamics
     Incompressible Flows Around Airfoils Of Infinite Span
  In Section 3 of this course you will cover these topics:
     Incompressible Flows About Wings Of Finite Span
     Dynamics Of A Compressible Flow Field
     Compressible, Subsonic Flows And Transonic Flows
  In Section 4 of this course you will cover these topics:
     Two-Dimensional Supersonic Flows Around Thin Airfoil
     Supersonic Flows Over Wings And Airplane Configurations
     Hypersonic Flows
  In Section 5 of this course you will cover these topics:
     Aerodynamic Design Considerations
     Tools For Defining The Aerodynamic Environment

Why Choose New York Metropolitan University

New York Metropolitan University is the name of excellence, and we emphasize fully working on the future of our students just so they can reach their true potential. Our unparalleled campus experience allows students of all races and religions to excel in their abilities. Here, you are not just growing in your educational career; you can also focus on and enhance your extracurricular activities. We are passionate about providing you with the best overall experience before you enter your professional career path. However, the real career paths of students begin with us.